View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 39026U 12072A 18112.57408919 +.00001813 +00000-0 +70479-4 0 9992
2 39026 097.2127 124.8327 0040064 158.0640 202.2326 15.26566660297115
Epoch (UTC): | 22 April 2018 13:46:41 |
Eccentricity: | 0.0040064 |
inclination: | 97.2127° |
perigee height: | 458 km |
apogee height: | 513 km |
right ascension of ascending node: | 124.8327° |
argument of perigee: | 158.0640° |
revolutions per day: | 15.26566660 |
mean anomaly at epoch: | 202.2326° |
orbit number at epoch: | 29711 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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